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JH-7 (Flounder) Chinese Fighter/Bomber

JH-7

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Basic Information
Name
JH-7 (Flounder) Chinese Fighter/Bomber
Designation
JH-7
Alternate Designation
Equipment Type
Manufacturer
Xi'an Aircraft Industry Corporation
Date of Introduction
1992
Description

The Xi'an JH-7 (NATO reporting name Flounder), also known as the FBC-1 (Fighter/Bomber China-1) Flying Leopard, is a tandem two-seat, twin-engine fighter-bomber in service with the People's Liberation Army Naval Air Force (PLANAF), and the People's Liberation Army Air Force (PLAAF). The main contractors are Xi'an Aircraft Industrial Corporation (XAC) and the 603rd Aircraft Design Institute (later named the First Aircraft Institute of AVIC-I). The first JH-7s were delivered to the PLANAF in the mid-1990s for evaluation, with the improved JH-7A entering service in 2004. In the early 1970s, the PLAAF required a new fighter-bomber to replace the Harbin H-5 and Nanchang Q-5. A request was duly submitted to the Ministry of Aviation Industry (later renamed to the Aviation Industry Corporation of China), which organized a domestic development program when efforts to secure a joint venture with foreign partners failed. The program was authorized on 19 April 1983 by then-paramount leader Deng Xiaoping. The program was also aiming to make use of newly imported British Rolls-Royce Spey turbofan engines at the time. The PLANAF required a similar aircraft and the program set out to develop a variant for each set of requirements. The PLAAF variant would be a two-man all-weather deep strike bomber, with side-by-side cockpit seating, electronic countermeasures (ECM), and terrain following capabilities similar to the General Dynamics F-111. The PLANAF would receive a two-man all-weather, tandem cockpit, strike and reconnaissance aircraft. The PLAAF variant was dropped in the early 1980s, with the PLANAF variant becoming the JH-7. Six prototypes were built by December 1988, and the PLANAF received 12 to 18 aircraft in the early 1990s for evaluation. The first aircraft used imported Rolls-Royce Spey Mk.202 engines, later replaced by a license-built copy, the WS-9. They were equipped with the Type 243H multifunction radar, which could detect ships at a maximum of 175 kilometers (109 mi), and MiG-21-sized aerial targets at 75 kilometers (47 mi). The JH-7 was designed as an anti-shipping fighter-bomber. As with the later JH-7A, its aerial combat capability was insignificant given the large number of specialist aircraft for that role.

Air & Air Defense Specifications
Crew 2
Engine licensed Rolls Royce Spey Mk 202
Cruise Speed 903.0 km/h
Range 3100.0 km
Wingspan 12.80 m
Variants
JH-7 Initial production version of the PLANAF anti-shipping fighter-bomber.
JH-7A Later production utilising composite structure to reduce weight, improved flying control system and improved avionics including the JL10A Shan Ying J-band pulse-Doppler radar. Weapon loads increased by the addition of two more wing hardpoints and two hardpoints under the intake trunking for mission pods such as targeting pods.
JH-7E Possibly export variant, shown at 2018 Zhuhai Airshow.
FBC-1 Flying Leopard Export version of the JH-7.
FBC-1A Flying Leopard II Export version of the JH-7A.
System
Alternate Designation(s) Xi'an JH-7; Flounder; FBC-1 Flying Leopard.
Primary Function / Type Fighter-Bomber
Manufacturer Xi'an Aircraft Industry Corporation
Crew 2
Number of Engines 2
Number of Hard Points 9 in total (6× under-wing, 2× wing-tip, 1× under-fuselage) with a capacity of 9,000 kg (20,000 lb) external fuel and ordnance,
Note The JH-7 was designed as an anti-shipping fighter-bomber.
Dimensions
Length 21.00 m
Height 6.22 m
Wingspan 12.80 m
Wing Area 52.3 m sq
Wheel Base 7.80 m
Wheel Track 3.06 m
Empty Weight INA
Takeoff Weight 27,415 kg
Automotive
Engine Name 2 x Xian WS9 turbofan
Number of Engines 2
Engine Type licensed Rolls Royce Spey Mk 202
Engine Power, Dry 55.83 kN each
Engine Power, Afterburner 91.26 kN each
Maximum Speed at Altitude 1,808 km/h at 1,000 m max
Cruise Speed 903 km/h
Maximum Range 3,100 km w/full internal fuel, full external fuel, no weapons
Radius 900 km
Ceiling 16,000 m
Takeoff Roll 920 m
Landing Roll 1,050 m
Main Gun System
System
Name Gryazev-Shipunov GSh-23
Type Autocannon
Caliber 23mm
Length 1,537 mm
Barrel Length 1,000 mm
Weight 50 kg
Barrels 2
Action Gast principle
Rate of Fire 3,400–3,600 rounds/min
Muzzle Velocity 715 m/s
Ammunition
Type Autocannon
Caliber 23mm
Cartridge 23x115 mm
Basic Load 1,500 Rounds
Main Missile Systems
Air-to-Air Missiles (Options) PL-5; PL-8' PL-9; PL-12
Anti-Ship Missiles (Options) Yingji-8K; Yingji-82K
Air-to-Surface Missiles (Options) CM-802A; KD-88; C-705; C-704
Anti-Radiation Missiles (Options) Yingji-91; LD-10; CM-102
Main Missile System #1
Name C-802
Type Anti-Ship Cruise Missile
Manufacturer China Aerospace Science and Industry Corporation
Length INA
Diameter INA
Weight INA
Warhead 190 kg high-explosive fragmentation
Engine French TRI 60-2 turbojet
Operational Range 125 km
Maximum Speed Mach 0.9
Guidance System Inertial navigation/active radar homing terminal guidance
Main Missile System #2
Name C-801
Type Anti-Ship Cruise Missile
Length 5.81 m
Diameter INA
Weight 815 kg
Warhead Weight 165 kg
Engine Rocket
Propellant solid rocket
Operational Range 42 km
Flight Altitude 5-7 m
Maximum Speed Mach 0.9
Guidance System Inertial navigation/active radar homing terminal guidance
Bomb Weapon Systems
Laser Guided Bombs (Options) GB1; GB5
Satellite Guided Bombs LS-6; FT-12; GB6; FT-2; FT-3; FT-6
Fire Control / Avionics
Radar Eagle Eye 232H multi-role pulse-Doppler
Fire Control Radar INA
Laser Desingator INA
Autopilot triplex digital-analog
Air Data Computer Type 8145
Radio Altimeter WG-5A
Navigation 210 Doppler
EW Radar Warning RW1045 receiver
Active Jamming 960-2 noise system
Passive Jamming 914-4G system
Protection
Stealth Properties INA
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin China
Category Multirole Aircraft
Air > Multirole Aircraft
Filter Label
J
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
21 m
Width
Height
6.22 m
Weight
27415 kg
Operators (1)
China
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